Flight determination of the aerodynamic stability and control characteristics of the NASA SGS 1-36 sailplane in the conventional and deep stall angles-of-attack of between -5 and 75 degrees
By: by Faramarz A. Mahdavi, Dral R. Sandlin
Contributors: Sandlin, Dral R; United States. National Aeronautics and Space Administration
Series: NASA contractor report -- NASA CR-176962
Publisher: California Polytechnic State University, Aeronautical Engineering Dept.; National Aeronautics and Space Administration; National Technical Information Service, distributor
Published: 1984
Place of publication: San Luis Obispo, Calif; [Washington, DC; Springfield, Va
Language: eng
Format: Microform
Notes: Distributed to depository libraries in microfiche

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1986] 2 microfiches